Mobile refrigeration system and control

ABSTRACT

A mobile refrigeration system that includes an engine that is operable at a first speed greater than zero and a second speed greater than zero. A compressor is operable in response to the engine at a first speed and a second speed. The system also includes an evaporator, a first temperature sensor positioned to measure a first temperature, and a second temperature sensor positioned to measure a second temperature. A controller is operable to transition the engine between the first speed and the second speed in response to the first temperature exceeding a first predetermined value and the second temperature falling below a second predetermined value.

RELATED APPLICATIONS

This application is a divisional of co-pending U.S. application Ser. No.10/930,635, filed Aug. 31, 2004, the entire contents of which is herebyincorporated by reference.

BACKGROUND

The present invention relates to a mobile refrigeration system. Moreparticularly, the present invention relates to an engine-driven mobilerefrigeration system that includes an automatic control system.

Mobile refrigeration systems are often used to chill or cool a storagearea within a mobile container, such as a truck trailer. Often,perishable items, such as fruits and vegetables, are transported usingthese systems. The shelf life and appearance of these products isgreatly affected by the temperature at which they are maintained duringshipping. For example, too low a temperature can cause freezing, whichdamages some of the products being shipped. Too high of a temperaturemay cause spoilage or rotting of some products that are shipped.

New trailers are getting larger and include less insulation. Inaddition, the insulation in old trailers degrades over time.Furthermore, trailers are commonly used across a wide ambienttemperature range, thus requiring precise temperature control across amuch wider capacity range. As such, current transport systems havedifficulty maintain the temperature of the products within a narrowrange without excess engine operation. The excess engine operationresults in additional engine and other component wear, additionalmaintenance, and additional fuel costs.

SUMMARY

The present invention provides a mobile refrigeration system thatincludes an engine that is operable at a first speed greater than zeroand a second speed greater than zero. A compressor is operable inresponse to the engine at a first speed and a second speed. The systemalso includes an evaporator, a first temperature sensor positioned tomeasure a first temperature, and a second temperature sensor positionedto measure a second temperature. A controller is operable to transitionthe engine between the first speed and the second speed in response tothe first temperature exceeding a first predetermined value and thesecond temperature falling below a second predetermined value.

The invention also provides a mobile refrigeration system that includesan engine that is operable at a first speed and a second speed. Acompressor is operable in response to operation of the engine to producea flow of compressed refrigerant. A valve is associated with thecompressor and is movable between a first position and a second positionto vary the flow of compressed refrigerant. A fan is operable inresponse to operation of the engine to produce a flow of air. A firsttemperature sensor is positioned to measure a first temperature and asecond temperature sensor is positioned to measure a second temperature.A timer is operable to time a duration and a microprocessor-basedcontroller is operable to vary the valve position to maintain the firsttemperature at about a user set point. The controller is also operableto transition the engine between the first speed and the second speed inresponse to a measured first temperature in excess of a firstpredetermined value and the second measured temperature less than asecond predetermined value and a timed duration greater than apredetermined time.

The invention also provides a method of controlling a mobilerefrigeration unit. The method includes operating an engine at a firstspeed and operating a compressor at a first speed in response to engineoperation to produce a flow of compressed refrigerant. The methodfurther includes measuring a first temperature and moving a valve inresponse to the measured first temperature to maintain the firsttemperature at about a first user defined temperature. The method alsoincludes measuring a second temperature and transitioning the engine toa second speed greater than the first speed in response to the measuredsecond temperature. The method further includes moving the valve inresponse to the second temperature to maintain the second temperature atabout a second user defined temperature.

BRIEF DESCRIPTION OF THE DRAWINGS

The description particularly refers to the accompanying figures inwhich:

FIG. 1 is a schematic illustration of a mobile refrigeration compartmentincluding a refrigeration system;

FIG. 2 is a schematic illustration of a refrigeration cycle;

FIG. 3 is a simplified flowchart illustrating a portion of the operationof the refrigeration system of FIG. 1;

FIG. 4 is a flowchart illustrating a portion of the operation of therefrigeration system of FIG. 1; and

FIG. 5 is a ladder diagram illustrating various temperaturerelationships.

Before any embodiments of the invention are explained, it is to beunderstood that the invention is not limited in its application to thedetails of construction and the arrangements of components set forth inthe following description or illustrated in the following drawings. Theinvention is capable of other embodiments and of being practiced or ofbeing carried out in various ways. Also, it is to be understood that thephraseology and terminology used herein is for the purpose ofdescription and should not be regarded as limiting. The use of“including,” “comprising,” or “having” and variations thereof is meantto encompass the items listed thereafter and equivalence thereof as wellas additional items. The terms “connected,” “coupled,” and “mounted” andvariations thereof are used broadly and encompass direct and indirectconnections, couplings, and mountings. In addition, the terms“connected” and “coupled” and variations thereof are not restricted tophysical or mechanical connections or couplings.

DETAILED DESCRIPTION

With reference to FIG. 1, a cargo space 10 such as would be found withina truck trailer is illustrated. The cargo space 10 includes a floor 15,a ceiling 20, two side walls 25, a front wall 30, and a rear wall 35.Generally, the rear wall 35 includes a door that allows for convenientloading and unloading of the cargo space 10. In most constructions, thewalls 25, 30, 35 the floor 15, and the ceiling 20 are insulated to maketemperature control of the cargo space 10 more efficient.

A refrigeration system 40 is attached to the outside of the front wall30 with other locations being possible. The refrigeration system 40draws relatively warm air from within the cargo space 10, cools the air,and returns the cold air to the cargo space 10. The front wall 30 of thecargo space 10 includes a return air aperture 45 that provides for thepassage of air from the cargo space 10 into the refrigeration system 40.Generally, a bulkhead 50 that may include an air filter at leastpartially defines the aperture 45.

Cold air exiting the refrigeration system 40 is generally directed to anair delivery duct 55 disposed on the ceiling 20 of the cargo space 10.The air delivery duct 55 distributes the cold air substantially evenlythroughout the cargo space 10 to assure that the entire cargo space 10is evenly cooled.

With reference to FIG. 2 the components of the refrigeration system 40are illustrated. Before describing the system 40, it should be notedthat many components, including valves, sensors, tanks, manifolds, andthe like have been omitted from the diagram for clarity.

The refrigeration system 40 includes a diesel engine 60 that functionsas the prime mover for the system. In other constructions, other engines(e.g., gasoline, Stirling, combustion turbine, hybrid, and the like) maybe used as the prime mover. The refrigeration system 40 also includes acompressor 65 that is driven by the engine 60 to produce a flow ofcompressed refrigerant (e.g., R12, freon, ammonia, etc.). The engine 60drives the compressor 65 such that the compressor 65 operates at a speedthat is proportional to the speed of the engine 60. In manyconstructions, a belt or chain drive 70 is employed to couple the engine60 and the compressor 65. However, other constructions may employ adirect drive, a gear drive, or another type of coupling or transmission.Many types of compressors can be employed including, but not limited to,screw compressors, reciprocating compressors, and scroll compressors.

The compressor 65 draws refrigerant from a suction line 75 andcompresses the refrigerant to produce a flow of compressed refrigerant.The compressed refrigerant flows to a condenser 80 where excess heat isremoved. The condenser 80 includes a heat exchanger that transfers heatenergy from the compressed refrigerant to an air stream 85. A condenserfan 90, driven by the engine 60, moves the air stream 85 through thecondenser 80 to facilitate the efficient removal of heat. As with thecompressor 65, preferred constructions employ a belt or chain drive 95between the condenser fan 90 and the engine 60 that assures that thecondenser fan 90 operates at a speed that is proportional to the speedof the engine 60. In other constructions, different coupling means suchas gears, direct drives, or other types of transmissions may be employedto allow the engine 60 to drive the condenser fan 90.

As the flow of compressed refrigerant passes through the condenser 80,the refrigerant generally condenses to a liquid state. The high-pressureliquid next flows to an expansion valve 100 where the pressure isreduced, thereby also reducing the temperature of the refrigerant. Thecold refrigerant then flows into an evaporator 105.

The evaporator 105 includes a second heat exchanger that transfers heatenergy from a second air stream 110 that is drawn from the cargo space10 to the refrigerant. Thus, the evaporator 105 cools the second airstream 110. As with the condenser 80, the evaporator 105 includes anevaporator fan 115 that is driven by the engine 60. The evaporator fan115 moves the second air stream 110 through the evaporator 105 and backinto the cargo space 10 to facilitate the efficient cooling of the airstream 110. As with the condenser fan 90, preferred constructions employa belt or chain drive 120 between the evaporator fan 115 and the engine60 that assures that the evaporator fan 115 operates at a speed that isproportional to the speed of the engine 60. In other constructions,different coupling means such as gears, direct drives, or other types oftransmissions may be employed to allow the engine 60 to drive theevaporator fan 115.

After the refrigerant leaves the evaporator 105, it returns to thesuction line 75 that feeds the compressor 65, thus completing the cycle.As one of ordinary skill in the art will realize, many other componentsmay be employed in the system just described. For example, multiplecompressors 65, evaporators 105, condensers 80, evaporator fans 115, orcondenser fans 90 could be employed in one system if desired. Inaddition, storage tanks, reservoirs, liquid-to-suction heat exchangers,economizers, unloader valves, and hot-gas bypass valves could beemployed at various points within the system.

With continued reference to FIG. 2, the refrigeration system 40 alsoincludes a suction line throttle valve 125. The suction line throttlevalve 125 moves between a first, or closed position and a second, oropen position. In the closed position, the valve 125 restricts thequantity of refrigerant delivered to the compressor 65 and thus reducesthe cooling capacity of the refrigeration system 40. As the valve 125moves toward the open position, additional refrigerant is able to passthrough the valve 125 to increase the cooling capacity of therefrigeration system 40. In most constructions, the valve 125 iselectrically controlled and actuated. However, other constructions mayemploy other types of valves (e.g., mechanically controlled andactuated) if desired. Other constructions may also employ valves thatare positioned differently than the suction line valve 125 (e.g.,unloader valves) but that still function to control the cooling capacityof the refrigeration system 40 by varying the flow of refrigerant to orfrom the compressor 65.

In some constructions, a third heat exchanger 130 is positioned adjacentthe evaporator 105 or actually intermingles with the evaporator 105. Thethird heat exchanger 130 receives a flow of heated fluid that can beused to defrost the evaporator 105. For example, one construction of therefrigeration system 40 directs engine coolant from the engine 60through the third heat exchanger 130 to periodically defrost theevaporator 105.

The system 40 includes a controller 135 that is interconnected with theengine 60 and a plurality of sensors to monitor and control therefrigeration system 40. In preferred constructions, amicroprocessor-based controller is employed. However, otherconstructions may employ an analog electric control system such as aseries of switches and relays or another controller (e.g., mechanicalcontrol system, PLC based system, and the like) as desired. The use ofthe microprocessor-based controller allows for greater flexibility andmore accurate control than what could be achieved using other types ofcontrollers.

Among the many sensors that may be employed, the refrigeration systemgenerally includes a return air sensor 140 that measures the temperatureof the air returning from the cargo space 10. Generally, the return airtemperature provides a good indication of the actual temperature of theproduct being shipped within the cargo space 10. Another sensortypically employed is a discharge air temperature sensor 145. Thedischarge air temperature sensor 145 measures the temperature of the airleaving the evaporator 105. Generally, this is the lowest airtemperature within the system 40. In many systems 40, redundant sensors140, 145 are provided such that the failure of one or more sensors doesnot disable the entire refrigeration system 40.

In most constructions, the refrigeration system 40 also includes a valveposition sensor 150. The valve position sensor 150 measures the actualposition of the valve 125 and returns a signal to the controller 135that is representative of the actual valve position. While manydifferent types of sensors or feedback are possible, LVDTs (linearvariable differential transformers) and RVDTs (rotational variabledifferential transformers) are preferred. In other constructions, astepper motor is used to drive the valve 125 and the position of thestepper motor is monitored using software, thus eliminating the need forposition feedback.

The refrigeration system 40 described herein is capable of operating inseveral modes depending on the operating conditions of the system 40 aswell as ambient conditions outside of the cargo space 10. In addition,the controller 135 is able to automatically transition the system 40between the various modes.

One mode of operation illustrated in FIG. 3 is return air control withmodulation. In this mode, the controller 135 monitors the return airtemperature (RAT) (shown in block 155) and manipulates the suction linethrottle valve 125 in an effort to maintain the measured return airtemperature at or near a user defined return air set point value T1.Generally, the user defined return air set point temperature T1 isbetween about 15 degrees and 90 degrees Fahrenheit. Of course, colder orwarmer temperatures could be selected if desired. As the throttle valve125 opens, more refrigerant is drawn into the compressor 65, therebyincreasing the cooling capacity of the refrigeration system 40. However,the air flow through the evaporator 105 remains substantially constantas the evaporator fan 115 moves at a constant speed. Thus, the airexiting the evaporator 105 is cooler. This air temperature is measured(at block 155) as the discharge air temperature (DAT).

To further improve the control of the temperature within the cargo space10, a lower limit is placed on the discharge air temperature whenoperating in return air control. This limit is generally referred to asthe discharge air floor limit T2. The discharge air floor limit T2 isgenerally determined by subtracting a user input deltaT (ΔT) value fromthe user defined return air set point value T1. For example, if a userselects a return air set point T1 of 40 degrees Fahrenheit and furtherselects a deltaT value of 5 degrees Fahrenheit, the discharge air floorlimit T2 would be 35 degrees Fahrenheit. In most constructions, a deltaTvalue between about 1 degree and 6 degrees Fahrenheit is preferred.However, other constructions may employ larger or smaller deltaT values.

If, during return air control operation, the discharge air temperaturefalls to the floor limit T2, the controller 135 automaticallytransitions the system 40 to discharge air temperature control (DATControl) shown in block 160. When in discharge air temperature control,the controller 135 manipulates the suction line throttle valve 125 in aneffort to maintain the discharge air temperature at the floor limit T2.

When controlling based on discharge air temperature, it is possible forthe return air temperature, and the cargo temperature to continue torise above the return air setpoint T1 due to many factors (e.g., highambient temperature, warm product, product respiration, airinfiltration, insulation degradation, evaporator airflow restrictions,and the like). The controller 135 monitors the return air temperatureand compares this temperature to a maximum temperature set point T3.Generally, the maximum temperature set point T3 is simply an offset 161from the return air set point temperature T1. For example, a particularload may have a return air set point T1 of 40 degrees Fahrenheit and anoffset of 5 degrees Fahrenheit. For this load, the maximum temperatureset point T3 would be 45 degrees Fahrenheit. If the return airtemperature exceeds the maximum temperature set point T3 for apredetermined length of time (e.g., 30 minutes) as measured by a timer163 or the controller 135, the system 40 automatically transitions tohigh-speed modulation (shown in block 165). In many constructions, thetimer is built into software, thus allowing the controller to performthe function of the timer.

In high-speed modulation, the engine speed is increased. During normaloperation the engine 60 operates at a first speed. The first speedprovides enough power, airflow, and sufficient temperature control tooperate the refrigeration system 40 under normal load conditions.However, under some load conditions additional power and airflow isrequired. Thus, the engine 60 is able to operate at a second speed thatis higher than the first speed. At the second speed, the evaporator fan115 and condenser fan 90 also operate at a higher speed. As such, bothfans 90, 115 are able to push additional air through the respective heatexchangers 80, 105. Similarly, the compressor 65 operates at a higherspeed, thereby enabling the compressor 65 to deliver a greater quantityof refrigerant if necessary.

During high-speed modulation, the controller 135 continues to manipulatethe suction line throttle valve 125 to maintain the discharge airtemperature at the floor limit T2. However, because additional air ismoving through the evaporator 105, the system 40 is able to maintain asubstantially constant cooling capacity, while reducing the temperaturedifferential between the discharge air temperature and the return airtemperature. The reduction in the temperature difference between thedischarge air and the return air is a result of the additional mass flowof air exiting the evaporator 105 at the floor limit temperature T2, ascompared to the mass flow when the engine 60 is operating at low speed.This additional air flow has the effect of reducing the return airtemperature.

The system 40 includes two conditions that facilitate the return tolow-speed modulation from high-speed modulation. If either of theseconditions is met, the system 40 transitions back to low-speedoperation. The first condition occurs when the return air temperaturereaches a switch point T4 that is equal to the return air temperatureset point T1 plus an offset 166 (see block 170). Generally, an offset166 of between about 1 and 10 degrees Fahrenheit is employed with largeror smaller offsets being possible. For example, if the return air setpoint T1 is set at 40 degrees Fahrenheit and an offset 166 of 5 degreesFahrenheit is employed, the switch point T4 would equal 45 degreesFahrenheit.

It should be noted that the maximum temperature set point T3 isgenerally offset a fixed amount 167 from the switch point T4. In mostconstructions, a 2-degree Fahrenheit offset is employed with larger orsmaller offsets being possible. The 2-degree offset reduces thelikelihood of sudden transitions between high and low speed in responseto minor temperature fluctuations. The relationships between thesevarious temperatures are best illustrated in FIG. 5.

The second condition is based on an integral error that accumulateswithin the controller (block 175). When the integral error reaches amaximum integral error value, the system transitions into low-speedmodulation. The integral error accumulates based on the temperaturedifference between the measured return air temperature and apredetermined value (e.g., the return air temperature set point T1 plusan offset, such as 2 degrees Fahrenheit). However, unlike a typicalintegral error, the integral error accumulates more slowly the greaterthe temperature error. Thus, a condition that maintains a hightemperature error (e.g., 10 degrees Fahrenheit) will take longer toreach the maximum integral error than would a condition that maintains asmall temperature error (e.g., 2 degrees Fahrenheit). Thus, the integralerror will allow the system 40 to operate at high-speed for a longerperiod of time if the temperature error is large, but will transitionthe system 40 back to low speed more quickly for small temperaturedifferences. For example, a simple refrigeration system may sum theinverse of the actual error to calculate an integral error. In thisexample, a constant error of 2 degrees Fahrenheit would produce an errorof 2 degree-minutes, per minute that the error is maintained. Theinverse of this value would produce an integral error of 0.5 that wouldincrease by 0.5 each minute. The same system, operating with a 10-degreetemperature error would produce an integral error of 0.1 that wouldincrease by 0.1 each minute. Thus, in this example it would take fivetimes longer to reach a maximum integral error value with a 10 degreeerror than it does with a 2 degree error.

The integral error assures that the system 40 will eventually transitionback to low speed operation no matter the temperatures being measured.This reduces the likelihood that the system 40 will operate at highspeed for a long period of time when low-speed operation would becapable of handling the cooling load.

Freeze protection, a portion of which is illustrated in FIG. 4, is yetanother mode of operation of the refrigeration system 40. When operatingin freeze protection, the floor limit T2 is calculated as an offset froma base level of 35 degrees Fahrenheit (block 180), rather than as anoffset from the return air set point temperature T1 (block 185). Thus,the user input deltaT value is subtracted from 35 degrees Fahrenheitwhen operating in freeze protection mode. This mode is particularly wellsuited for use when the cargo space 10 contains high-temperature setpoint goods. For example, if the return air temperature set point T1 is45 degrees Fahrenheit and the delta T value is 3 degrees, the floorlimit would be 42 degrees Fahrenheit without using freeze protection.With freeze protection, the floor limit would be 32 degrees Fahrenheit(i.e., 35 degrees −3 degrees). The lower floor limit T2 in freezeprotection mode allows the system 40 to remain in low-speed modulationduring operating conditions that would otherwise require high-speedmodulation. The reduced high-speed operation saves engine fuel andreduces engine wear.

It should be noted that the fixed value of 35 degrees Fahrenheit used infreeze protection could vary from system to system. As such, theinvention should not be limited to a fixed value of 35 degreesFahrenheit.

During operation of the refrigeration system 40, cold refrigerantflowing within the evaporator 105 will cool the evaporator 105. If theevaporator 105 cools below about 32 degrees Fahrenheit, water vaporwithin the air stream 110 will condense and freeze onto the evaporator105. As this process continues, the air flow paths through theevaporator 105 will shrink due to the expanding quantity of ice. Thereduced air flow through the evaporator 105 reduces the cooling capacityof the refrigeration system 40 but also reduces the discharge airtemperature. When operating in modulation with return air control, thereduced air flow caused by the ice build-up will result in a rise inreturn air temperature. Simultaneously, the reduced air flow paths willproduce a drop in discharge air temperature. At some point, thesetemperature changes will transition the system 40 into discharge aircontrol. Once in discharge air control, the controller 135 willmanipulate the suction line throttle valve 125 to maintain the dischargeair temperature at the floor limit T2. However, as the air flow pathcontinues to shrink, the discharge air temperature will continue todrop. The continued drop will cause the controller 135 to move thesuction line throttle valve 125 to a more closed position even as thereturn air temperature rises. It is this combination of a reduction indischarge air temperature coupled with an increase in return airtemperature and the movement of the suction line throttle valve 125toward the closed position (block 190 in FIG. 3) that signals the needfor a defrost cycle (block 195). The controller 135 senses theseconditions and initiates the defrost cycle. Most systems also include anevaporator coil temperature sensor 200 that can also be used to indicatethe need for a defrost cycle and the end of the defrost cycle. Asdiscussed, there are various ways to defrost an evaporator 105 (e.g.,passing hot engine coolant or refrigerant through the third heatexchanger 130, electric heat, etc.), the particular system or methodused is not important to the invention described herein.

After the defrost cycle is complete, the controller 135 transitions thesystem 40 to one of the low-speed modulating control modes (e.g., returnair control or discharge air control).

The refrigeration system 40 described is able to maintain thetemperature within the cargo space 10 within a narrow temperature bandthat is selected by the user, while also reducing the operating time ofthe engine 60 at high speed. The result is a system that requires lessmaintenance than prior systems and that is more fuel-efficient. Inaddition, the improved temperature control results in improved qualityof the product being shipped.

It should be noted that many systems may include an electric motor thatserves as a back-up to the engine. In most constructions, a single-speedelectric motor is used. However, other constructions may employ atwo-speed or variable speed motor if desired.

High speed modulation gives the user the ability to control both thedischarge air temperature (i.e., the floor limit) and the maximum returnair temperature at the same time. Prior systems could only regulate onetemperature. Furthermore, the temperature control can be customized forthe particular load by the selection of various set points andtemperature differentials. This allows the user to balance thetemperature requirements with the amount of high-speed runtime. Thus, auser could select a wider temperature band to reduce the amount ofhigh-speed operation and the amount of fuel consumed if desired. Thecontrol as described is able to provide consistent temperature controlregardless of the product hauled, the operating conditions, or thetrailer condition.

Although the invention has been described in detail with reference tocertain preferred embodiments, variations and modifications exist withinthe scope and spirit of the invention as described and defined in thefollowing claims.

1. A method of controlling a mobile refrigeration unit comprising:operating an engine at a first speed; operating a compressor at a firstspeed in response to engine operation to produce a flow of compressedrefrigerant; measuring a first temperature; moving a valve in responseto the first temperature to maintain the first temperature at about afirst user defined temperature; measuring a second temperature;transitioning the engine to a second speed greater than the first speedin response to the measured second temperature; and moving the valve inresponse to the second temperature to maintain the second temperature atabout a second user defined temperature.
 2. The method of claim 1,wherein the engine includes a diesel engine.
 3. The method of claim 1,wherein the first temperature is a return air temperature.
 4. The methodof claim 1, wherein the second temperature is a discharge airtemperature.
 5. The method of claim 1, wherein the transitioning stepincludes: comparing the first temperature to a user defined maximumtemperature; calculating a duration that the first temperature remainsabove the user defined maximum temperature; and transitioning the enginespeed when the first temperature remains above the user defined maximumtemperature for a duration that is greater than a user defined timeperiod.
 6. The method of claim 1, further comprising calculating themaximum temperature by adding an offset value to the first user definedtemperature.
 7. The method of claim 1, further comprising controllingthe valve position to maintain the second temperature at a user definedfloor limit when the second temperature falls at or below the floorlimit.
 8. The method of claim 7, further comprising calculating the userdefined floor limit by subtracting a user defined deltaT from the firstuser defined temperature.
 9. The method of claim 8, wherein the userdefined deltaT is between about 1 degree and 6 degrees Fahrenheit. 10.The method of claim 7, further comprising calculating the user definedfloor limit by subtracting a user defined deltaT from a fixedpredetermined value.
 11. The method of claim 10, wherein the fixedpredetermined value is about 35 degrees Fahrenheit and the user defineddeltaT is between about 1 degree and 6 degrees Fahrenheit.
 12. Themethod of claim 1, further comprising initiating a defrost cycle inresponse to a first air temperature in excess of a predetermined value,a second air temperature at or below a predetermined value, and movementof the valve toward a position that reduces a flow of refrigerant. 13.The method of claim 1, further comprising positioning an evaporatoradjacent a cooled space and positioning a defrost member adjacent theevaporator.
 14. The method of claim 13, wherein the defrost memberincludes a defrost heat exchanger.
 15. The method of claim 14, whereinthe controller directs a flow of fluid to the defrost heat exchanger inresponse to the measured first temperature exceeding a value, themeasured second temperature falling below a second value, and movementof the valve toward a position that reduces a flow of refrigerant. 16.The method of claim 1, further comprising transitioning the engine fromthe second speed to the first speed in response to one of the firstmeasured temperature falling below a switch point value, and a summationof an integral error exceeding a predetermined maximum integral error.17. The mobile refrigeration system of claim 16, wherein the integralerror is inversely proportional to a temperature error.